首页|期刊导航|交通信息与安全|基于前轮转角补偿的牵引车-飞机系统运动学模型及轨迹跟踪控制方法

基于前轮转角补偿的牵引车-飞机系统运动学模型及轨迹跟踪控制方法OACSCD

A Kinematic Model and Trajectory Tracking Control of Tractor-Aircraft System Based on Front Wheel Angle Compensation

中文摘要英文摘要

传统的牵引车-飞机系统运动学模型在低速滑行牵引工况下精度不足,导致轨迹跟踪控制误差大、响应慢,难以满足新型离港方式对轨迹精度和安全性的高要求.为提升运动学模型精度与轨迹跟踪性能,研究了基于牵引车前轮转向角补偿函数的运动学模型补偿方法.以威海广泰AM210无杆牵引车和B737-800飞机为研究对象,先建立传统的牵引车-飞机系统运动学模型,然后将传统运动学模型与Trucksim车辆模型进行开环联合仿真对比分析,通过引入补偿函数来补偿2种模型之间的轨迹偏差,同时设计了基于非线性模型预测控制(nonlinear model predictive control,NMPC)的牵引车-飞机系统轨迹跟踪控制器.以双移线工况作为参考轨迹,搭建MATLAB/Simulink与Trucksim闭环联合仿真模型,并将NMPC控制器与传统比例积分微分控制(pro-portional integral derivative,PID)的轨迹跟踪控制器进行轨迹仿真对比分析,验证NMPC控制器的优越性.进一步在2 m/s和4 m/s牵引车速度下分别对基于传统、补偿后的运动学模型的NMPC控制器跟踪性能进行评估并且分析存在不同初始偏差下对牵引车-飞机系统轨迹跟踪性能的影响.仿真结果显示:在2 m/s和4 m/s牵引车速度下基于补偿后的运动学模型的NMPC控制器可以使跟踪峰值误差分别降低61.93%和41.63%,均方根误差分别降低56.14%和37.69%.在存在的初始偏差情况下,基于NMPC的轨迹跟踪控制器能够使系统在30s内完成对初始偏差(横向偏差0.5~1 m、航向角偏差0.05~0.1 rad)的修正,无超调现象.

The traditional kinematic model of the tractor-aircraft system exhibits insufficient accuracy under low-speed taxiing towing conditions,resulting in significant trajectory tracking control errors and slow responses,which is difficult to meet the stringent requirements for trajectory accuracy and safety for the new departure mode.To improve the accuracy of the kinematic model and the performance of trajectory tracking,this study proposes a ki-nematic model compensation method based on a front wheel steering angle compensation function of the tractor.Taking the Weihai Guangtai AM210 rodless tractor and the B737-800 aircraft as research objects,a traditional kine-matic model of the tractor-aircraft system is first established.Then,the traditional kinematic model and the Truck-sim vehicle model are subjected to open-loop joint simulation and comparative analysis.The trajectory deviations between these two models are compensated by introducing a compensation function.Meanwhile,a trajectory track-ing controller for the tractor-aircraft system based on nonlinear model predictive control(NMPC)is designed.Tak-ing the double-shifting line condition as the reference trajectory,a closed-loop joint simulation model utilizing MAT-LAB/Simulink and Trucksim is built,and the trajectory simulation comparison and analysis between the NMPC con-troller and the traditional proportional-integral-derivative control trajectory tracking controller are conducted to veri-fy the superiority of the NMPC controller.The tracking performance of the NMPC controller based on the tradition-al and compensated kinematic models is further evaluated at tractor speeds of 2 m/s and 4 m/s respectively,and the influence of different initial deviations on the trajectory tracking performance of the tractor-aircraft system is ana-lyzed.The simulation results show that the NMPC controller based on the compensated kinematic model can reduce the peak tracking error by 61.93%and 41.63%,and the root mean square errors by 56.14%and 37.69%,at tractor speeds of 2 m/s and 4 m/s,respectively.Under the condition of existing initial deviations,the trajectory tracking con-troller based on NMPC can enable the system to correct the initial deviations(lateral deviation of 0.5 to 1 m and heading angle deviation of 0.05 to 0.1 rad)within 30 s without overshoot.

孙艳坤;颉鑫龙;张威

中国民航大学航空工程学院 天津 300300中国民航大学航空工程学院 天津 300300中国民航局中国民航航空地面特种设备研究基地 天津 300300||中国民航局民航智慧机场理论与系统重点实验室 天津 300300||中国民航大学科技创新研究院 天津 300300

航空航天

智能交通牵引车-飞机系统补偿函数运动学模型轨迹跟踪

intelligent transportationtractor-aircraft systemcompensation functionkinematic modeltrajectory tracking

《交通信息与安全》 2025 (5)

79-92,14

国家自然科学基金民航联合基金重点项目(U2033208)、中央高校基本科研业务费项目(3122020031)资助

10.3963/j.jssn.1674-4861.2025.05.008

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